P/N: 212-060-208-001
Category: Structural Components
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| Condition | Price | Stock |
|---|---|---|
| As Removed | $250.00 | 2 Available |
The 212-060-208-001 is a structural fitting designed to join and reinforce aircraft airframe members at critical load-transfer points. Manufactured from aircraft-grade metal to OEM specifications, this component supports fuselage frame attachments and bracket installations. Installation requires precise fitting and torquing per the applicable structural repair manual or maintenance data to ensure continued airworthiness and load-carrying capability.
Used in general aviation and commercial aircraft structural assemblies.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 212-060-208-001 is a structural fitting designed to join and reinforce aircraft airframe members at critical load-transfer points. Manufactured from aircraft-grade metal to OEM specifications, this component supports fuselage frame attachments and bracket installations.
The FITTING may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the FITTING. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 212-060-208-001.